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Calculation of the longitudinal stability derivatives of a transport aircraft and analysis of longitudinal modes

  • Uǧur Özdemir*
  • , Elbrous M. Jafarov
  • , Mehmet Ş Kavsaoǧlu
  • *Bu çalışma için yazışmadan sorumlu yazar

Araştırma sonucu: Kitap/Rapor/Konferans Bildirisinde BölümKonferans katkısıbilirkişi

5 Atıf (Scopus)

Özet

In this study, the longitudinal stability derivatives of a transport aircraft have been calculated by modeling the aircraft configuration and flight condition. The applying method is able to use for all sizes of civil and military aircrafts. As a second step, the longitudinal motion of aircraft is investigated and the transfer functions of linearized equations of motion have been obtained. Phugoid and short period modes have been investigated. Frequency-response and transient-response analysis have been performed respectively by using Matlab Simulink.

Orijinal dilİngilizce
Ana bilgisayar yayını başlığıProceedings of the 9th WSEAS International Conference on Automatic Control, Modeling and Simulation, ACMOS '07
Sayfalar105-110
Sayfa sayısı6
Yayın durumuYayınlandı - 2007
Etkinlik9th WSEAS International Conference on Automatic Control, Modeling and Simulation, ACMOS '07 - Istanbul, Turkey
Süre: 27 May 200729 May 2007

Yayın serisi

AdıProceedings of the 9th WSEAS International Conference on Automatic Control, Modeling and Simulation, ACMOS '07

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???event.eventtypes.event.conference???9th WSEAS International Conference on Automatic Control, Modeling and Simulation, ACMOS '07
Ülke/BölgeTurkey
ŞehirIstanbul
Periyot27/05/0729/05/07

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